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Parallel Computational Fluid Dynamics 2006 by A. Ecer, N. Satofuka, Pat Fox, Jacques Periaux, Jang-Hyuk Kwon

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Numerical Analysis of Supersonic Jet Flow from Vertical Landing Rocket Vehicle in Landing Phase

Toshiyuki Suzukia; Satoshi Nonakab; Yoshifumi Inatanib    a Institute of Aerospace Technology, JAXA 7-44-1 Jindaiji-Higashi-machi, Chofu, Tokyo 182-8522, Japanb Institute of Space and Astronautical Science, JAXA 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510, Japan

Keywords

Large Eddy Simulation

Opposing Jet

1 INTRODUCTION

As a future space transportation system, a working group at Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA) proposed a concept of a fully reusable launch vehicle.1 The proposed vehicle is a single stage vertical taking off and landing (VTOL) type one. For the purpose of verification of ...

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